SL-12 R/B(2), 19400

Orbit data source: Space-Track

SL-12 R/B(2), 19400 is space debris in GEO originally from a launch on Thu, 18 Aug 1988 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.

Not visible in the next 10 days
Identifier
19400, 1988-071D
Orbit
GEO
Country
Flag of CISCIS
Related business
Manufacturer
NPO Energiya
Mission
Spacecraft
Bus & Motor
BLOK DM, Unknown motor
Mass
2,440 kg wet, 2,440 kg dry
Launch date (UTC)
1988-08-18 (38 years ago)
Launch vehicle
Unknown
Launch site
Tyuratam Missile And Space Complex (TTMTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Cyl, 3.1 m
Radar Cross Section
23.597 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 3 days ago

TLE from 3 days ago
0 SL-12 R/B(2)
1 19400U 88071D   26154.87581587 -.00000356  00000-0  00000-0 0  9990
2 19400  11.2723 329.1535 0018772 241.0044 116.5917  1.00546372132565
Epoch: 2026-06-03T21:01Z
TLE epoch observation values (Epoch: 2026-06-03T21:01:10.491Z)
Latitude
-0.43291°
Longitude
119.33933°
Altitude
35,744.501 km
Speed
3.075 km/s
True Right ascension
21h 47m 50s
True Declination
0° 25' 57"
Sunlit
Object was in daylight at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
03:23:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
35,789.815 km
Perigee altitude
35,631.796 km
Semi-major axis
42,088.943 km
Eccentricity
0.00188
Inclination
11.2723°
RAAN
329.1535°
Arg. of periapsis
241.0044°
True anomaly
116.78385°
Mean anomaly
116.5917°
Eccentric anomaly
116.6878°
Mean motion
0.25136 °/min
Orbital period
1,432.23 mins
BSTAR
0
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